The design and assembly of joint between outer wing and center wing is essential for the developing commercial aircraft. Five kinds of joints for upper panel between outer wing and center wing were researched in this article. CATIA models were established. Using the finite element calculation, the stress and strain condition of the same load was obtained. Comparation and analysis were given from loading, manufacturing and weight, in order to get the advantages and disadvantages of the different joints. The research could provide a technology support for civil aircraft structure design.